TM 1-1520-238-23
4-549
4.163.
NO. 1 AND NO. 2 POWER AVAILABLE SPINDLE CABLE SUPPORT BRACKET
REMOVAL/INSTALLATION (PILOT TO CPG) – continued
4.163.4. Cleaning
a. Clean removed and attaching parts (para
1.47).
4.163.5. Inspection
a. Check support bracket for cracks. None al-
lowed.
b. Check support bracket for corrosion (para
1.49).
c. Check support bracket for damaged nut
plates (TM 1-1500-204-23). None allowed.
4.163.6. Installation
a. Install support bracket (1) on airframe (2).
(1) Position support bracket (1).
(2) Install two screws (5) through washers (4),
bracket (6), and support bracket (1).
(3) Install two washers (4) and nuts (3) on two
screws (5).
b. Inspect (QA).
c. Install No. 1 engine power available spindle
cable (pilot to CPG) (para 4.159).
d. Install No. 2 engine power available spindle
cable (pilot to CPG) (para 4.161).
END OF TASK
M04-3928-3
3
4
4
6
5
1
2
